Modular Casing for High-Speed Imaging Equipment
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Solution Overview
Problem
Existing sensing equipment, particularly imaging apparatus, faces challenges when operating in high stress environments such as high-speed aircraft, where it must withstand harsh conditions like high accelerations, pressures, and vibrations, leading to costly and inefficient operations due to the need for specialized and inflexible camera pods that increase pilot workload and require extensive maintenance.
Innovation Solution
A modular casing system for sensing apparatus that includes detachable sections with a cylindrical shape for aerodynamic performance, adaptable mounting options, and integrated load-carrying structures, allowing for flexible deployment on various vehicles and environments, while incorporating pressure relief valves and optically transparent materials for imaging.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Adaptability or versatility
If a single-body camera pod is used, then the structure is simple and inexpensive, but the adaptability to different aircraft and environments is poor
Solution Approach 1:
The camera pod is divided into multiple detachable sections (nose section, body section, tail section) that can be assembled and disassembled. This segmentation allows the same modular components to be configured for different aircraft types and mission requirements, significantly improving adaptability while maintaining reasonable structural complexity through standardized interfaces.
Solution Approach 2:
The modular casing sections are designed with universal mounting interfaces and standardized connection mechanisms that can be used across different aircraft platforms. The same basic sections can serve multiple functions by reconfiguration, allowing one set of components to adapt to various aircraft types and imaging requirements.
2Reliability
If camera pods are heavily modified for specific functions, then the imaging capability is optimized, but the maintenance requirements and cost increase
Solution Approach 1:
By segmenting the camera pod into standardized sections with detachable connections, the system allows easy replacement of individual components without affecting the entire structure. This reduces maintenance complexity and cost, as only the specific malfunctioning section needs to be serviced or replaced rather than the entire customized pod.
Solution Approach 2:
The modular design enables individual sections to be independently replaced, recovered, or upgraded. Worn or damaged sections can be discarded and replaced with new or refurbished modules, reducing overall maintenance requirements and allowing selective replacement based on actual wear or performance needs rather than complete system overhaul.
3Adaptability or versatility
If existing aircraft pods are modified to accommodate cameras, then the imaging equipment can be mounted, but the original design compromises and pilot workload increase
Solution Approach 1:
The modular casing is designed with universal mounting interfaces that can attach to various aircraft types without requiring extensive custom modifications to the host aircraft. This universality reduces the operational complexity and pilot workload by providing a standardized system that works across different platforms without requiring aircraft-specific procedures or adjustments.
4Measurement precision
If high-speed imaging equipment is used, then the imaging quality is improved, but the film consumption and maintenance requirements increase
Solution Approach 1:
The modular design allows the imaging system to use disposable or easily replaceable film/ sensor modules that can be quickly exchanged after use. High-speed imaging sections can be replaced rather than serviced, reducing maintenance downtime and allowing efficient handling of high film consumption rates through standardized replacement procedures rather than complex maintenance operations.
Data Source
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AI summary
Casings (100) and housings for use in high speed airflow (for example for mounting on a high speed vehicle) are described. In one embodiment, a housing for imaging equipment is described. The housing has a tapering form with symmetrical angular truncations such that it tapers in the form of a wedge with two substantially planar regions. At least one substantially planar region comprises an aperture formed of optically transparent material.